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由于输入到操纵战术导弹的自动驾驶仪,需要视线角误差速率,通常采用陀螺稳定的接收器以跟踪目标。由控制和误差转矩产生陀螺进动角速率,误差转矩是由伺服进动放大器-转矩产生器组件和由其它各种转矩产生机构引起的。进动放大器的输出作为自动驾驶仪的输入信号。磁偶极子、由陀螺转子和接收器组成装置受控制(进动)电流的影响,该电流通过陀螺周围的螺线圈,这种进动电流的大小和相位,控制转子的进动速率的大小和方向。当陀螺稳定接收器跟踪目标时,进动放大器提供一种与惯性视线角误差速率成比例的信号。导出控制装置的动力学方程式;结果解释直轴和横轴弹性速率效应(在实验室观察的)。通常认为陀螺自旋马达的垂直转矩效应看作是由若干现象引起的。讨论实验过程确定方程系数,并估价动力学误差源的相关量,根据现有情况确定机械装置和性能改进,以使进动放大器误差源减到最少并完全消除其它的误差源。
Due to the autopilot of maneuvering tactical missiles, which requires a line-of-sight error rate, a gyro-stabilized receiver is often used to track the target. Gyro precession angular velocity is generated by control and error torques, which are caused by servo preamplifier-torque generator components and by various other torque-producing mechanisms. The precession amplifier output is used as the autopilot input signal. The magnetic dipole, which is composed of the gyro-rotor and receiver components, is controlled by the precession current, which is passed through the solenoid around the gyroscope. The magnitude and phase of this precession current controls the magnitude of the precession rate of the rotor And direction. When the gyro-stabilized receiver tracks the target, the precession amplifier provides a signal that is proportional to the rate of error of the inertial line-of-sight error. The kinetic equations of the control device are derived; the results explain the effects of the elastic velocity of the straight and transverse axes (observed in the laboratory). It is generally considered that the vertical torque effect of the gyro-spin motor is caused by several phenomena. Discuss the experimental process to determine the coefficient of the equation, and estimate the relative amount of kinetic error sources, based on the current situation to determine the mechanical devices and performance improvements to minimize the preamplifier error sources and completely eliminate other sources of error.